Space systems — Re-entry risk management for unmanned spacecraft and launch vehicle orbital stages — Amendment 1: Formula to obtain Ec by the product of the probability of impact on a specific latitude band, and the population within the band, which is integrated over the latitude range covered by the orbital inclination
STANDARD published on 8.9.2020
Designation standards: ISO 27875:2019-ed.2.0/Amd1:2020
Note: Change
Publication date standards: 8.9.2020
The number of pages: 1
Approximate weight : 3 g (0.01 lbs)
Country: International technical standard
Category: Technical standards ISO